>*OLGHU ÀDSV@
AIL to RUD
7KLV PL[ LV XVHG ZKHQ \RX ZDQW WR FRRUGLQDWH
WKH UXGGHU ZLWK DLOHURQ RSHUDWLRQ IRU EDQNLQJ DW
VKDOORZ DQJOHV >$LUSODQHJOLGHU JHQHUDO@
RUD to AIL
7KLV IXQFWLRQ LV XVHG ZKHQ \RX ZDQW WR PL[
WKH DLOHURQV ZLWK UXGGHU LQSXW 5XGGHU LV DSSOLHG
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>$LUSODQHJOLGHU JHQHUDO@
CAMBER MIX
7KLV PL[ DGMXVWV WKH FDPEHU DQG FRUUHFWV WKH
HOHYDWRUV >$LUSODQHJOLGHU DLOHURQV RU PRUH@
ELE to CAMBER
7KLV PL[ LV XVHG ZKHQ \RX ZDQW WR WKH PL[
FDPEHU ÀDSV ZLWK HOHYDWRU WR LQFUHDVH WKH OLIW RI WKH
PRGHO >$LUSODQHJOLGHU DLOHURQV RU PRUH@
CAMB.FLP to ELE
This mix is used to correct for changes in attitude
ZKHQ WKH FDPEHU IODSV DUH XWLOL]HG >$LUSODQH
JOLGHU DLOHURQV ÀDS RU PRUH@
%877(5)/< &URZ
7KLV IXQFWLRQ LV XVHG WR TXLFNO\ VORZ WKH DLUFUDIW
DQGRU UHGXFH WKH DOWLWXGH >*OLGHU DLOHURQV RU
PRUH )O\LQJ DLOHURQV ÀDS RU PRUH@
TRIM MIX
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FDQ EH DFFHVVHG E\ VHOHFWLQJ D VZLWFK RU FRQGLWLRQ
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RUDDER 1
Winglet
(
)
at Flying wing
AIL 3
(Chip Aileron)
ELEVATOR
(RUDDER 2)
AIRBRAKE
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ÀLJKW $LUSODQH DLOHURQV RU PRUH
GYRO
LV XVHG >$LUSODQHJOLGHU JHQHUDO@
V-TAIL
UXGGHU LQSXW IRU XVH ZLWK 9WDLO PRGHOV >$LUSODQH
JOLGHU 9WDLO VSHFL¿FDWLRQV@
$,/(9$725 '8$/ (/(9$725
RI PRGHOV ZLWK HOHYDWRU VSHFLILFDWLRQV >$LUSODQH
JOLGHU DLOHYDWRU VSHFL¿FDWLRQV@
WINGLET
RI ZLQJOHW PRGHOV >$LUSODQHJOLGHU ZLQJOHW
VSHFL¿FDWLRQV@
MOTOR
WKH PRWRU RI DQ )% RU RWKHU VXFK (3 JOLGHU LV
VWDUWHG E\ D VZLWFK >$LUSODQHJOLGHU JHQHUDO@
RUD to ELE
VXFK DV NQLIH HGJH ÀLJKW >$LUSODQH JHQHUDO@
SNAP ROLL
DGMXVWV WKH DPRXQW RI VHUYR LQSXW 6HUYR VSHHG FDQ
DOVR EH DGMXVWHG >$LUSODQH JHQHUDO@
FLP 4
AIL1
FLP 3
(Brake Flap)
(Brake Flap)
(Main Aileron)
FLP 1
(Camber Flap)
AILVATOR
V-TAIL
RUDDER
ELEVATOR
(ELEVATOR 2)
(AILERON 5)
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7KLV IXQFWLRQ LV XVHG ZKHQ DLUEUDNHV DUH
7KLV LV D GHGLFDWHG PL[ ZKHQ D *<$ 6HULHV J\UR
This function incorporates the elevators and
7KLV IXQFWLRQ DGMXVWV WKH HOHYDWRUV DQG DLOHURQV
7KLV IXQFWLRQ DGMXVWV WKH OHIW DQG ULJKW UXGGHUV
7KLV IXQFWLRQ DGMXVWV WKH RSHUDWLRQ VSHHG ZKHQ
This function is used to correct rolling maneuvers
7KLV IXQFWLRQ VHOHFWV WKH VQDS UROO VZLWFK DQG
RUDDER 2
AIL 2
(Main Aileron)
Winglet
(
at Flying wing
AIL 4
FLP 2
(Camber Flap)
(Chip Aileron)
ELEVATOR 2
(AILERON 6)
)
85